Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft /

Bibliographic Details

Main Authors:	Berrier, Bobby L. (Author), Re, Richard J. (Author)
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Series:	NASA technical paper ; 1766.
Subjects:	Convergent-divergent nozzles. Mach number. Nozzle design. Performance tests. Pressure ratio.
Online Access:	https://purl.fdlp.gov/GPO/gpo71372